TX-261

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Model: ARPAT-2. Thrust (vac): 244.000 kN (54,853 lbf). Burn time: 11 sec. Propellants: Solid. Diameter: 0.71 m (2.32 ft). Length: 3.10 m (10.10 ft). Country: USA. No Engines: 1. Motor: TX-261-3. Status: Retired 1965. Used as: Pedro. Release conditions: Thiokol. Used on Launch Vehicles: ARPAT. Contact us with any corrections, additions, or comments. Conditions for use of drawings, pictures, or other materials from this site.. To contact astronauts or cosmonauts. © Mark Wade, 1997 - 2008 except where otherwise noted.